Suspended Load Path Tracking by a Tilt-rotor UAV

被引:1
|
作者
Rego, Brenner S. [1 ]
Raffo, Guilherrae V. [2 ]
机构
[1] Univ Fed Minas Gerais, Grad Program Elect Engn, BR-31270901 Belo Horizonte, MG, Brazil
[2] Univ Fed Minas Gerais, Dept Elect Engn, BR-31270901 Belo Horizonte, MG, Brazil
来源
IFAC PAPERSONLINE | 2016年 / 49卷 / 32期
关键词
Tilt-rotor UAV; Load Transportation; Path Tracking Control; State Estimation; TRANSPORTATION;
D O I
10.1016/j.ifacol.2016.12.220
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper deals with the load transportation problem by a tilt-rotor unmanned aerial vehicle. Most approaches address the subject by formulating the system dynamics from the UAV's point of view, with the load's behavior described with respect to it. Difficulties arise if control tasks are given for the load, since the suspended load coordinates do not appear explicitly in the mathematical formulation. A novel approach is proposed, based on the formulation of the system dynamics using position and orientation of the load as generalized coordinates. The equations of motion are developed in detail, yielding a highly coupled state-space representation. It is shown that linear techniques are sufficient for path tracking of the load at low accelerations, even when subject to external disturbances and incomplete, noisy information about the state vector is available. Simulation results are presented in order to validate the proposed approach. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
收藏
页码:234 / 239
页数:6
相关论文
共 50 条
  • [21] Load alleviation for a tilt-rotor aircraft in airplane mode
    Manimala, B
    Padfield, GD
    Walker, D
    JOURNAL OF AIRCRAFT, 2006, 43 (01): : 147 - 156
  • [22] A tilt-rotor actuator
    White, G.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2010, 224 (G6) : 657 - 672
  • [23] A new robust adaptive mixing control for trajectory tracking with improved forward flight of a tilt-rotor UAV
    Cardoso, Daniel N.
    Esteban, Sergio
    Raffo, Guilherme, V
    ISA TRANSACTIONS, 2021, 110 : 86 - 104
  • [24] Back-stepping Control Strategy for Stabilization of a Tilt-rotor UAV
    Chowdhury, Arindam Bhanja
    Kulhare, Anil
    Raina, Gaurav
    PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 3475 - 3480
  • [25] Transition Strategy Optimization of Tilt-Rotor VTOL UAV in Conversion Process
    Sun, Hao
    Zhou, Zhou
    Wang, Zhengping
    Dong, Qiyuan
    PROCEEDINGS OF THE 2021 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY (APISAT 2021), VOL 2, 2023, 913 : 1057 - 1077
  • [26] Finite-Time Control Design for a Coaxial Tilt-Rotor UAV
    Lv, Zongyang
    Zhao, Qing
    Sun, Xi-Ming
    Wu, Yuhu
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2024, 71 (12) : 16132 - 16142
  • [27] Tracking Control for a Tilt-rotor with Input Constraints by Robust Gaits
    Shen, Zhe
    Tsuchiya, Takeshi
    2023 IEEE AEROSPACE CONFERENCE, 2023,
  • [28] European tilt-rotor concept
    Birch, S
    AEROSPACE ENGINEERING, 2000, 20 (09) : 6 - 6
  • [29] TILT-ROTOR PROSPECTS ARE ON THE RISE
    HANLEY, A
    AEROSPACE AMERICA, 1987, 25 (10) : 6 - 8
  • [30] Tilting Curve Design of a Novel Tilt-rotor UAV Based on Rotor/Wing Interference Model
    Huang, Huaping
    Yu, Li
    He, Guang
    Wang, Xiangke
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 2356 - 2361